Ce projet de doctorat est aux prises avec un problème de ruptures en fatigue de un alliage de titane aéronautique en raison de haute fréquence chargement. Matériel pour cette enquête a été prise de compresseur du moteur disque de l'avion réel. Essais de fatigue à ultrasons ont été réalisées jusqu'à dépasser la limite de 1010 cycles. Cette région de la durée de vie est connu comme Gigacycle ou fatigue très grand nombre de cycles. Ce projet de thèse montre pour la première fois les résultats des tests de fatigue sur l'lliage de titane aéronautique VT3-1 dans la région Gigacycle. Les propriétés de fatigue de l'alliage de titane ont été déterminées à 109 cycles pour les conditions de chargement différentes: traction-compression, tension-tension et de torsion. Mécanismes d'initiation des fissures typiques ont été identifiés et des défauts critiques de microstructure ont été trouvés. L'effet de l'anisotropie en raison de processus de fabrication sur les propriétés de fatigue de l'alliage de titane VT3-1 forgé a été étudiée. Une influence du processus de fabrication sur les propriétés de fatigue a également été étudiée par comparaison les résultats sur extrudé et forgé VT3-1 alliage de titane. La nouvelle machine de torsion à ultrasons a été conçu et installé pour la longue durée de vie (jusqu'à 1010 cycles) de tests de fatigue en rotation. Les premiers résultats sous la chargement en torsion ultrasons ont été obtenues pour l'alliage de titane réalisé par extrusion et technologies forgés. / This PhD project is dealing with a problem of fatigue failures of aeronautical titanium alloy due to high frequency loading. The material for investigation was taken from the real aircraft engine compressor disk. Ultrasonic fatigue tests were carried out up to outrun limit of 1010 cycles. This region of lifetime is known as Gigacycle or very high cycle fatigue. This PhD project shows for the first time the results of fatigue tests on the VT3-1 aeronautical titanium alloy in the Gigacycle region. The fatigue properties of the titanium alloy were determined at 109 cycles for different loading conditions: tension-compression, tension-tension and torsion loading. Typical crack initiation mechanisms were identified and critical defects of microstructure were found. The effect of anisotropy due to fabrication process on the fatigue properties of the forged VT3-1 titanium alloy was studied. An influence of technological process on fatigue properties was also studied by comparison the results on extruded and forged VT3-1 titanium alloy.The new ultrasonic torsion machine was designed and installed for the long life (up to 1010 cycles) fatigue tests under rotation. The first results under ultrasonic torsion loading were obtained for the titanium alloy made by extrusion and forged technologies.

Cette étude s’est focalisée sur l’influence d’une opération de fraisage sur l’intégrité de surface et la durée de vie en fatigue des pièces usinées en titane (Ti-6Al-4V). L’influence des paramètres géométriques tels que les angles de coupe et les rayons de bec sur la performance de l’outil à savoir la durée de vie de l’outil est analysée. Une deuxième partie est consacrée à l’influence des paramètres géométriques sur l’intégrité de surface définie par des facteurs tels que la topographie, les contraintes résiduelles, la dureté et la microstructure. Afin de déterminer la nature des contraintes résiduelles, une approche thermomécanique a été utilisée. Une relation entre les contraintes résiduelles et la dureté sous la surface usinée est établie. Une dernière partie est dédiée à la l’étude de la fatigue des pièces en titane usinées selon les différents paramètres géométriques. Une comparaison des limites d’endurance expérimentales et analytiques issue de la littérature a permis de déterminer les paramètres influents de l’intégrité de surface sur la performance en fatigue. Une analyse fractographique a révélé les phénomènes liés à l’usinage influençant la rupture du matériau. / This study is carried out on the influence of milling process on surface integrity and fatigue life of a titanium alloy (Ti-6Al-4V). Geometric parameters like cutting angles and nose radius are investigated. In the first part, the observation is focused on tool life. The second part is dedicated to the influence of geometric parameters on surface integrity which is defined by topography, residual stress, hardness and microstructure. To determine the nature of the residual stresses a thermomechanical approach is used. A relation between residual stress and hardness is established. The last part deals with the study of the fatigue of milled titanium samples. A comparison is made between experimental fatigue limit and analytical fatigue limit of a model from literature. With this comparison, the most influential factor of surface integrity on fatigue limit is determined. A fractography analysis reveals the phenomenon related to milling process which can influence the material rupture.

Les alliages de titane β métastables sont des matériaux de structure essentiels pour les applications aéronautiques de part leurs très bonnes propriétés mécaniques. En effet, ils présentent une résistance spécifique élevée, une bonne ductilité et forgeabilité et une excellente réponse aux traitements thermiques. Toutefois, il existe encore aujourd'hui à leur sujet des controverses et des questions ouvertes et ce, malgré les efforts pour comprendre les mécanismes d'évolution microstructurale au cours de traitements thermo-mécaniques et pour déterminer les phases en présence et leur contribution aux les propriétés mécaniques résultantes. Ce travail de thèse a pour objectif de déterminer la nature de la phase β et de caractériser la transformation β→α à haute et basse températures par des caractérisations fines en microscopie électronique à balayage et à transmission couplées à des mesures d'orientations cristallographiques et de composition chimique. L'alliage étudié est un Ti-5553 avec une microstructure initiale 100% β obtenue par mise en solution et trempe. Il a été démontré expérimentalement que la structure de la phase β métastable n'est pas purement cubique centrée. Les points de la phase β dans les clichés de diffraction présentent un allongement (streaking) et des points supplémentaires sont visibles aux positions de diffraction 1/2, 1/3 et 2/3. Par ailleurs, les images MET ont un aspect en moiré. A partir de ces résultats et de calculs crystallographiques, il a été prouvé que des déplacements atomiques sur les plans {110}β et {112}β forment une structure intermédiaire entre celle de la phase β parente et celles des phases α et ω, prouvant que la phase β a intrinsèquement initié une transformation. L'étude de la précipitation au cours du procédé thermomécanique dans le domaine α+β a révélé que des précipités α discontinus, équiaxes ou légèrement allongés (1~2μm) se forment aux joints β de forte et de faible désorientation mais rarement au coeur des grains β produisant ainsi une microstructure en "collier". La relation d'orientation de Burgers (ROB) entre les phases α et β est progressivement détruite par la déformation. L'écart à la ROB est plus marqué pour les précipités α qui se forment au joint de grains qu'à l'intérieur des grains. L'écart à la ROB augmente aussi avec la déformation, mais diminue avec la vitesse de déformation. Au cours des déformations en bas du domaine α+β, les précipités α ont une morphologie qui dépend de leur position. Au coeur des bandes de glissement, les grains α/β sont équiaxes et ne respectent pas la ROB. Entre les bandes de glissement, la microstructure est lamellaire où les phases α/β alternent et respectent la ROB. Dans ce dernier cas, une forte sélection de variantes a été observée: Seuls les deux ou trois variants favorisant l'accommodation de la déformation se sont formés. A titre de comparaison, dans l'état non déformé, les 12 précipités sont présents. La transformation β→α est retardée en cours de compression à haute température. Ceci est attribué à une compétition entre adoucissement et transformation de phase. Au contraire, celle-ci est favorisée au cours de la compression à plus basse température du fait que les défauts cristallins induits par la déformation jouent le role de sites de germination et que la croissance des précipités soit accéléré alors que l'adoucissement soit ralenti. Dans le Ti-5553, le mécanisme de déformation dominant est le glissement des dislocations. Dans les déformations en bas du domaine α+β, du glissement simple ou multiple avec deux ou trois systèmes de glissement activés. L'identification de ces systèmes a pu être effectuée par des analyses de traces. Cette thèse a résolu la nature de la phase β métastable et constitue un travail de référence pour l'étude de la transformation β→α au cours de traitement thermomécanique / Metastable β titanium alloys are important structural materials for aeronautical applications due to their high strength to density ratio, good ductility and workability and excellent hardenability. Despite the efforts in resolving the complex microstructural evolution related to thermomechanical processes and in gaining knowledge on the produced phases and their contribution to the resultant mechanical properties, there are still some controversial and unresolved issues. The aim of the present PhD work is to determine precisely the metastable nature of β phase and to characterize finely the characteristics of the β→α transformation during high and low temperature thermomechanical treatments. Investigations were performed on a Ti-5553 alloy with the single β phase initial microstructure obtained by solution treatment followed by quenching using scanning and transmission electron microscopy (SEM/TEM) coupled to crystallographic orientation measurements and chemical analyses. It was demonstrated experimentally that the structure of the β phase in the metastable titanium alloy is not “pure” body centered cubic. Diffraction diagrams presents streaking of the β diffraction spots and additional spots at the 1/2, the 1/3 and 2/3 diffraction positions. Also, striations are observed in TEM images. From this experimental evidence and crystallographic calculations, it was proved that atomic displacements on the {110}β and {112}β planes formed a structure between that of the parent β phase and that of the α or ω phase, demonstrating pre-phase transformation tendency. The study of the precipitation during thermomechanical processing at higher temperature in the α+β region revealed that discontinuous equiaxed or short rod shaped α precipitates (1~2μm) mainly form on the high angle and low angle β grain boundaries but seldom in β grain interiors, forming the “necklace” microstructure. The Burgers orientation relationship (BOR) between the α and β phases is destroyed gradually by the deformation. The BOR deviation of grain boundary α is larger than that of intragranular α. The deviation from the BOR increases both with the increasing strain and decreasing strain rate. During the deformation at the lower temperature in the α+β region, the α precipitates exhibit different morphologies: such as lamellar α, equiaxed α and irregular α depending on their localization. Within the slip bands, equiaxed α/β grains which do not respect the BOR are present. However, between the bands, lamellar α and β phases maintaining the BOR are distributed alternately. In that last case a strong variant selection is observed as only the two or three variants that form are those which can accommodate the macroscopic deformation. Comparatively, in absence of compression all 12 variants are formed. The β→α phase transformation is retarded during the hot compression at higher temperature region, which is attributed to the competition between softening and phase transformation. On the contrary, it is promoted during compression at lower temperature region due to the more inducted deformation defects acting as α phase nucleation sites and due to accelerating growth of α precipitates and retarded softening. Dislocation slip is the leading deformation mechanism for the Ti-5553 alloy. Under the lower temperature deformation condition, single or multiple-slip bands with two or three different activated slip systems would form during the hot deformation process. Identification of these slip systems have been done by trace analysis. These results provide new insights into the structural nature of β metastable phase and valuable reference for β→α phase transformation during thermo-mechanical treatment in metastable β titanium alloys

La problématique initiale part du constat que les échecs d’implants sont souvent causés par une inadéquation entre les propriétés élastiques de l’os et celles de l’implant. Aujourd’hui, ce problème de biocompatibilité mécanique suscite un intérêt croissant et a conduit au développement d’alliages de titane β-métastables qui possèdent un module d’élasticité faible, moitié moindre que celui de l’alliage Ti-6Al-4V classiquement utilisé dans les applications d’implantologie. De plus, les structures architecturées ou treillis font, elles aussi, l’objet d’intenses recherches dans le but de réduire le module d’élasticité et de maximiser la résistance. Leur mise en forme, avec une maîtrise précise de l’architecture, est possible grâce à la fabrication additive et les nombreuses possibilités qu’elle offre : liberté de design, gain matière, pièces complexes, customisation de masse... Ce travail de thèse porte sur la mise en œuvre de l’alliage de titane à bas module d’élasticité Ti-26Nb(%at.) par la technologie de fusion laser sur lit de poudres. Une stratégie d’élaboration in situ de ces alliages à partir de poudres élémentaires de Ti et de Nb est explorée, à la fois pour permettre d’éventuels ajustements de composition, et pour pallier au manque de disponibilité des alliages de titane sous forme de poudres. La démarche est réalisée avec deux morphologies de poudre, irrégulière et sphérique. Les effets des nombreux paramètres de ce procédé (puissance du laser, vitesse et stratégie de balayage...) sur l’homogénéité et la porosité des pièces élaborées sont quantifiés. Un alliage homogène peut être obtenu sous réserve de l’utilisation d’une densité d’énergie adaptée et d’une granulométrie de poudre tenant compte des températures de fusion respectives des éléments. La caractérisation de la microstructure met en évidence une texture marquée, dépendante de la stratégie de balayage. Les pièces élaborées présentent un bas module d’élasticité associé à une résistance mécanique élevée, avec une déformation élastique favorable par rapport à un alliage de référence coulé. Par ailleurs, un algorithme d’optimisation est développé et permet de contrôler les propriétés mécaniques d’une structure architecturée à partir de ses paramètres géométriques (rayon, longueur et orientation des poutres). La combinaison de cet alliage de titane à bas module d’élasticité et d’une structure architecturée développée à partir ce cet algorithme a été appliqué à une prothèse totale de hanche, qui a fait l’objet de simulations par éléments finis. L’évaluation du phénomène de stress-shielding montre que, comparativement à un modèle massif plus rigide, ce type de prothèse permet de réduire de façon significative la déviation des contraintes. En se rapprochant du modèle dit physiologique, cette prothèse peut être qualifiée de « biomimétique » sur le plan du comportement mécanique / The initial problematic arises from the fact that implant failure is often caused by a mismatch between the elastic properties of the bone and those of the implant. Nowadays, an increasing interest is given to this mechanical biocompatibility and led to the development of β-metastable titanium alloys that possess low Young’s modulus, about half that of the conventionally used Ti-6Al-4V alloy. Moreover, lattice structures are currently being the subject of many investigations with the aim of achieving low Young’s modulus and high strength. Their fabrication, with accurate control over the architecture, is made possible thanks to additive manufacturing processes and the several possibilities they offer: design freedom, reduced material usage rate, complex shapes, mass customisation... The present work focuses on the implementation of low modulus titanium alloy Ti-26Nb(at.%) by the means of selective laser melting. An in situ elaboration strategy, based on a mixture of elemental powders, is explored in order to allow potential composition adjustments and to overcome the unavailability of titanium alloy powders. The approach is carried out using two distinct powder morphologies, spherical and irregular. The effects of the numerous parameters of the process (laser power, speed, scanning strategy...) on homogeneity and porosity of the manufactured parts is quantified. A homogeneous alloy can be obtained subject to the use of suitable energy density levels and powder size distributions that take into account the respective fusion temperatures of both elements. Microstructure characterisation highlights a pronounced texture resulting from the scanning strategy. The elaborated samples display a low Young’s modulus associated with a high strength, and hence a favourable strength to elastic modulus ratio compared to the reference cast alloy. Furthermore, an optimization algorithm is developed and allows controlling the mechanical properties of a lattice structure with its geometrical parameters (radius, length and orientation of struts). The combined use of this low Young’s modulus titanium alloy with a lattice structure developed through this algorithm was applied to the design of a total hip prosthesis that was subjected to finite element simulations. Stress-shielding evaluation shows that, compared to a solid design, this kind of prosthesis permits to reduce stress-shielding significantly. By getting closer to a physiological model, this prosthesis can be qualified as “biomimetic” in terms of mechanical behaviour

O presente trabalho visou determinar a tenacidade à fratura dinâmica, KID, primeiramente pelos conceitos da Mecânica da Fratura Elástica Linear (MFEL) e posteriormente pela Mecânica da Fratura Elasto-Plástica (MFEP), JID, em materiais que em operação podem estar sujeitos a impactos em diferentes temperaturas. Os materiais estudados, de uso na indústria aeronáutica, foram uma liga de titânio Ti6Al4V (norma SAE AMS 4911), na condição recozida e uma liga de aço inoxidável PH 15-5 (norma SAE AMS 5659), na condição H1000. Os corpos de prova pré-trincados e entalhados foram retirados nas orientações L-T e L-S, a fim de que fossem determinadas e comparadas a relação tenacidade/densidade ou tenacidade específica dos materiais estudados. Em seguida os corpos de prova foram ensaiados sob condições de carga dinâmica em uma máquina de ensaio Charpy instrumentado, marca Instron-Wolpert PW30, conforme a norma ASTM-E23, com velocidade de carregamento de 5,52 m/s e nas temperaturas de 23 e 400ºC. Os valores das tenacidades, posteriormente comparados e correlacionados, foram obtidos de acordo com as expressões matemáticas mencionadas na literatura. A razão entre as energias estimadas de iniciação (Ei) e de propagação (Ep), (Ei/Ep), foi obtida a partir dos gráficos de carga-deslocamento x tempo. A determinação e caracterização dos aspectos macro e microscópicos da fratura foram realizadas através de microscopia ótica e de varredura. Em seguida, confrontaram-se os valores e os aspectos preponderantes dos mecanismos de fratura apresentados por cada material. / The present work aimed to evaluate the dynamic fracture toughness, KID, firstly using the Linear Elastic Fracture Mechanics parameter, (LEFM), and secondly using the Elasto-Plastic Fracture Mechanics (EPFM), JID. The materials used in this work are from aeronautic grade and are subjected to in service impact loads and temperature variation. The materials are a titanium alloy Ti6Al4V (standard SAE AMS 4911), in the annealed condition and a PH 15-5 stainless steel (standard SAE AMS 5659), H1000 condition. Both precracked and notched specimens were taken in the L-T and L-S directions, for the evaluation and comparison of the toughness/density ratio, i. e., the specific dynamic fracture toughness of the materials studied. Therefore, the specimens were tested under dynamic load using an Instron-Wolpert PW30 Instrumented Charpy Equipment, following the ASTM-E23 standard, with load speed of 5,52 m/s at 23 and 400ºC. The fracture toughness values were compared using mathematical expression from literature. The ration between the initiation (Ei) and propagation (Ep) energies, (Ei/Ep), was obtained from the load-displacement x time. The characterization of the macro and microscopic aspects of the fracture mechanisms were carried out using optical microscope and scan electronic microscope. The fracture toughness values and the fractographic observations were correlated and compared for the two materials studied.

Alloys of titanium are highly preferred materials for their excellent strength to weight ratio but the tribological issues while using them has been posing challenging issues for the tribological analyst, which are still areas of active research. Ti-6Al-4V (Ti64) is the most popular alloy of titanium and our understanding of the fundamental mechanisms of wear and friction of this alloy is still not complete. Previous investigations related to the tribology of these alloys have suggested a synergistic effect of plastic deformation and tribo-oxidation. The present investigation described in this thesis explores the existence of one more mode, namely the formation of a Mechanically Mixed Layer (MML). The thesis examines the effect of these modes one by one and analyses the synergistic effect of these mechanisms, and also the effect of heat generation during sliding. The tribological condition existing have been varied by doing wear experiments using Ti64 pins sliding against alumina and SS316L (controls MML), diameter of pin (expected to control debris entrapment and thus MML formation), tribo-system (horizontal disc Vs vertical disc, which is also expected to control debris entrapment and thus MML formation), environment (ambient and vacuum, expected to control tribo-oxidation) and sliding speed (expected to control interface temperature and thus plastic deformation mechanism and tribo-oxidations). The division of the main chapters has been so made to present the findings spread over Chapters 5-8, with each chapter dealing with specific tribological test conditions. In each chapter, results from the tribological experimentations in the form of wear and friction are presented, together with the characterization methods which throw light into the tribological mechanisms. These characterization methods include Scanning Electron Microscopy (SEM), Energy Dispersive X-ray Spectroscopy (EDAX), X-Ray Diffraction (XRD) and Electron probe micro-analyzer (EPMA). Wherever possible, the debris collected from the experiments have been subjected to morphological and detailed chemical analysis, and a feature which has not been explored much in detail by tribological investigators, but having a promising potential. Experimental results from tribological testing when Ti64 pins slides against two different materials (Alumina and SS316L) in pin-on-disc tribometers under two different environmental conditions (ambient /vacuum) are analyzed. Each set of experiments looks at two different effects - (1) the effect of sliding speed on the tribological behavior while using a pin of a fixed diameter (all other parameters remaining the same) and (2) the effect of using pins of different diameters for a given set of parameters. Three different pin-sizes were employed (2.1 mm. 4.6 mm and 6.6 mm), the normal loads on these pins were changed according to the pin-size used so that all experiments were done at the same contact pressure (2.8 MPa). By performing the experiments against the ceramic disc (alumina) under vacuum conditions, the effect of this plastic deformation is studied in isolation because the possibility of the Tribo Chemical Reaction (TCR) due to oxidation is inhibited and no MML was found to be formed due to poor compatibility of mixing between the metallic pin and the ceramic disc. For the low speeds/strain rates experiments, the effect of plastic deformation as influenced by the adiabatic shear banding is seen to influence wear which progressively changes to temperature induced plastic deformation and wear. The situation is found to be different when we change the environmental conditions from vacuum to ambient for the same tribo-combination. The tests shows a reduction in wear rate with speed, and this is due to the oxide formations due to TCR as confirmed from the SEM/EDAX characterization. In contrast to previous experiments under vacuum, these permit the effect of TCR also to influence the tribological behavior. The scenario changes when the alumina disc is replaced by a metallic one (SS316L) and tests carried out in vacuum, as the MML was found to be formed with this tribo-pair. Because of the mutual affinity of the materials in the tribo-pair, the wear damage is severe in this case and the flash temperatures crossing the phase transition temperature (~880oC) for Ti64 at high speeds. The growth of the β phase with increase in the sliding (temperature) conditions is captured from the XRD spectra of the wear debris. Synergistic effect of all these mechanisms (plastic deformation, MML, and TCR) is permitted by conducting experiments with Ti64 pin against stainless steel and in ambient conditions. A comparison of the tribological response by presenting results when experiments are run over a range of speeds while using different sized pins under ambient conditions (and compared with similar results in vacuum) while using SS316L disc serve to demarcate the differences in the wear modes which are active/inactive depending on the tribological conditions. In addition a study incorporating the effect of frictional heating and its influence on the tribological phenomena is analyzed. Main conclusions from the thesis are: The wear resistance of Ti64 alloy when sliding against SS316L is found to be influenced by Strain Rate Response (SRR), Tribo Oxidation (TO), Mechanically Mixed Layer (MML) and the prevailing heat flux conditions at the contact. The wear rates were found to decrease marginally with sliding speeds (strain rates) up to a certain speed, which is ascribed to reduction in adiabatic shear band intensity with increase in strain rate. Adiabatic Shear Band (ASB), which allows easy crack propagation, intensity reduces as temperature of deformation of Ti64 is increased. From the results it can be confirmed that the propensity for formation of MML depends on compatibility of the disc and the pin material. The contribution due to of entrapment and retention of debris in the contact zone also would influence formation of the MML. The effect of frictional heating plays an influential role as it can affect the factors (TO, ASB, MML) governing the tribological response. The sensitivity to temperature, which is a marked feature of this alloy in undergoing softening, as confirmed by previous researchers, is reflected in the experimental results. Since the main factor that triggers the micro-structural instability is the energy dissipation that accompanies deformation more fundamental research which can improve the thermal transport properties of this alloy, would be the future scope of work of this thesis. Also, the unique composition of the MML which offers high wear resistance under specific operating conditions opens up the possibility of new such alloy formulations, production routes and techniques which should improve the tribological response of this alloy.

With the growing demands for bone implant therapy, titanium (Ti) and its alloys are considered as appropriate choices for the load-bearing bone implant substitutes. However, the interaction of bare Ti-based implants with the tissues is critical to the success of the implants for long-term stability. Thus, surface modifications of Ti implants with biocompatible hydroxyapatite (HAp) coatings before implantation is important and gained interest. Sol-gel is a potential technique for deposition the biocompatible HAp and has many advantages over other methods. Therefore, this review strives to provide widespread overview on the recent development of sol-gel HAp deposition on Ti. This study shows that sol-gel technique was able to produce uniform and homogenous HAp coatings and identified the role of surface pretreatment of Ti substrate, optimizing the sol-gel parameters, substitution, and reinforcement of HAp on improving the coating properties. Critical factors that influence on the characteristics of the deposited sol-gel HAp films as corrosion resistance, adhesion to substrate, bioactivity, morphological, and structural properties are discussed. The review also highlights the critical issues, the most significant challenges, and the areas requiring further research.

La technologie laser est couramment utilisée dans les industries aéronautiques depuis les années 1980. La découpe au laser, comme étant un procédé d’enlèvement de matière, offre plus d’avantages que les procédés conventionnels de la découpe. Parmi les apports du laser, l’absence de contact mécanique avec le matériau à usiner, une limitation de contamination des matériaux et une production élevée due à une haute vitesse de coupe. Les alliages de titane et les composites intermétalliques à base de titane jouent un rôle important dans le domaine de la science et de l’ingénierie ainsi ils permettent de satisfaire les activités de fabrication avancée dans les industries aéronautiques. L’amélioration de ce procédé de fabrication est souhaitable pour augmenter les performances techniques et accentuer l’intérêt économique. Les travaux réalisés ont porté sur l’étude et l’analyse des effets des paramètres de l’usinage par faisceau laser sur l’intégrité de la surface en termes de qualité et morphologie de la surface usinée de plusieurs matériaux, tels que, le titane pur, les alliages de titaneTi-6Al-4V et Ti6242 et le composite intermétallique à base de titane afin d’optimiser les conditions de découpage par laser.La sélection des paramètres de coupe dans le processus d’usinage laser tels que la puissance du laser, la vitesse de coupe, la pression du gaz d’assistance est importante pour assurer l’exactitude de l’usinage et l’amélioration de la microstructure, la rugosité, la zone affectée thermiquement, la largeur de la saignée, la micro dureté et le taux d’enlèvement de matière, résultant des sollicitations mécaniques et thermiques subies durant les différentes étapes de production.Cette étude se base sur une approche empirique faisant intervenir la méthodologie des plans d’expériences (ANOVA, Taguchi), la technique de la logique floue et les méthodes de décision multicritères (FTOPSIS, GRA) pour définir d’une façon rationnelle les essais expérimentaux visant à optimiser les conditions de découpe au laser dans le but de maximiser la production en assurant une meilleure qualité de fabrication. / Laser technology has been widely used in the aeronautics industry since the 1980s. Laser cutting, as a material removal process, offers more advantages than conventional cutting processes. Among the contributions of the laser, the absence of mechanical contact with the material, a limitation of contamination of the materials and a high production due to a high cutting speed. Titanium alloys and titanium-based intermetallic composites have an important role in the field of science and engineering, making it possible to satisfy advanced manufacturing activities in the aerospace industries. Improvement of this manufacturing process is desirable to increase technical performance and economic interest. The present framework focused on study and analysis of the effects of laser beam machining parameters on the surface integrity in terms of quality and morphology of several materials, such as pure titanium, titanium alloysTi-6Al-4V and Ti6242 and the titanium-based intermetallic composite to optimize laser cutting conditions.Selection of cutting parameters in the laser machining process such as laser power, cutting speed, assist gas pressure is important to ensure machining accuracy and microstructure , roughness, heat affected zone, kerf width, microhardness and rate of removal of material improvement, resulting from the mechanical and thermal stresses undergone during the different stages of production.This study is based on an empirical approach involving the experimental design methodology (ANOVA, Taguchi), the fuzzy logic technique and the multicriteria decision methods (FTOPSIS, GRA) aiming at optimizing laser cutting conditions in order to maximize production by ensuring better manufacturing quality.

The PhD thesis deals with the influence of temperature and strain rate on the mechanical behaviour of the Ti-6Al-4V titanium alloy. After verification tests under static loading conditions, the samples were deformed at high strain rates and elevated temperatures, using device for Hopkinson pressure bar test. The result is dependence of stress and strain rate on strain in the temperature range of 20 to 500°C. The deformed shape of specimen from the Taylor anvil test is compared with the results of the simulation in the Ansys – LS Dyna software. The parameters of Johnson-Cook equation were determined from these experiments. Also, the influence of loading conditions on the microstructure was studied. Both optical and scanning electron microscopes were used for the observations. During the research, some adjustments to the experimental devices were made in order to suppress the high-frequency components and noise in the recorded pulses. A functional tensile test adapter for the Hopkinson test was developed; it is registered under No. 2007/008 at the Technology Transfer Office of BUT.

Tato práce se zabývá pokročilou technologií výroby personalizovaných kloubních implantátů metodou EBM za použití titanové slitiny Ti6Al4V-ELI a navrhuje nový unikátní design kolenního implantátu společně s metodologií jeho inserce, přičemž tato řešení jsou součástí patentové přihlášky č. PV 2020-459. Toto neinvazivní řešení náhrady kolenního kloubu je šetrnější k pacientovi, maximálně chrání jeho zdravé tkáně a kosti, navíc se dá předpokládat vyšší životnost implantátu ve srovnání s tradičními dostupnými řešeními. Byla uskutečněna výroba vzorků z materiálu Ti6Al4V-ELI metodou EBM, proveden rozbor jejich materiálových, mechanických, technologických a únavových vlastností. Dále byly popsány pokročilé metody zobrazování, úpravy a tvorby kloubních ploch a použity k vyvinutí nového designu personalizovaného kloubního implantátu společně s inovační technologií jeho inserce a nástroji potřebnými k její úspěšné realizaci. Toto nové řešení bylo úspěšně ověřeno mnoha testy i výrobou Ti6Al4V-ELI a CoCrMo prototypů implantátů metodou EBM. Proveditelnost a použití v praxi bylo konzultováno a schváleno odborníky v této oblasti.